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Saturn LCB-Alumizine-140 stage
Part of Saturn LRB stage series
N2O4/Alumizine propellant rocket stage. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb payload to LEO): Low Cost Booster, Single Pressure-fed N2O4/Alumizine Propellant engine, HY-140 Hull.

AKA: Saturn LCB-Alumizine-140. Status: Study 1967. Thrust: 22,563.10 kN (5,072,387 lbf). Gross mass: 1,542,200 kg (3,399,900 lb). Unfuelled mass: 154,200 kg (339,900 lb). Specific impulse: 280 s. Specific impulse sea level: 260 s. Burn time: 166 s. Height: 36.28 m (119.02 ft). Diameter: 6.61 m (21.68 ft). Span: 9.26 m (30.38 ft).



Country: USA. Engines: PF N204/Alumizine-2300k. Launch Vehicles: Saturn LCB-Alumizine-140. Propellants: N2O4/Alumizine.

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